Discussion
An aerobatic aircraft is limited to \( +6 \) g. If it stalls at \( 40 \) m/s level, its corner speed is nearest to
Answer: C
Multiplying by the square root of the limit factor, \( 40 \times \sqrt{6} = 40 \times 2.449 = 98 \) m/s. The higher structural limit pushes the corner speed much further out than a transport's, which is exactly what makes tight aerobatic manoeuvres possible.
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